# Service difficulty reports: N246CA, cancelled Mar 30, 2001

A list on [N246CA, cancelled Mar 30, 2001](https://openairdocs.org/deregistered/N246CA-2001-03-30.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR COMA0010062](https://openairdocs.org/sdr/COMA0010062.md): Circuit Breaker · tripped · May 4, 2000 · N246CA · Emb EMB120RT · Electrical Power System
  > FLIGHT IDLE CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. PERFORMED OPS CHECKS WITH NO FAULTS.
- [SDR COMA0010019](https://openairdocs.org/sdr/COMA0010019.md): Computer · malfunctioned · Jan 29, 2000 · N246CA · Emb EMB120RT · Integrated Flight System
  > DURING TAKEOFF EHSI AND EADI, SCREENS WENT BLANK. COULD NOT DUPLICATE. REPLACED NR 2 AHRS FOR TROUBLESHOOTING.
- [SDR COMA9910168](https://openairdocs.org/sdr/COMA9910168.md): Battery · discharged · Oct 25, 1999 · N246CA · Emb EMB120RT · Emergency Lighting
  > FWD FLOOR PATH EMERGENCY LIGHTS ARE INOP. REPLACED THE NR 1 POSITION EMERGENCY BATTERY.
- [SDR COMA9910157](https://openairdocs.org/sdr/COMA9910157.md): Windshield · loose · Oct 3, 1999 · N246CA · Emb EMB120RT · Flight Compartment Windows
  > LOUD AIR NOISE FROM THE CAPTAINS WINDSHIELD AFTER DEPARTURE FROM MCO, AIRCRAFT RETURNED TO THE FIELD. RETORQUED THE SCREWS FOR THE CAPTAINS WINDSHIELD.
- [SDR COMA9910106](https://openairdocs.org/sdr/COMA9910106.md): Sign · missing · Jul 6, 1999 · N246CA · Emb EMB120RT · Emergency Lighting
  > EXIT SIGN AT ROW 5 IS MISSING. REPLACED EXIT SIGN.
- [SDR COMA9910050](https://openairdocs.org/sdr/COMA9910050.md): Light · inoperative · Mar 30, 1999 · N246CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY FLOOR LIGHT, ROW 2 IS INOPERABLE. REPLACED LIGHT.
- [SDR COMA9910010](https://openairdocs.org/sdr/COMA9910010.md): Bulb · failed · Jan 8, 1999 · N246CA · Emb EMB120RT · Emergency Lighting
  > FORWARD, RED, EMERGENCY FLOOR LIGHT IS INOPERABLE. REPLACED LIGHT BULB.
- [SDR COMA9810268](https://openairdocs.org/sdr/COMA9810268.md): Pcu · failed · Nov 13, 1998 · N246CA · Emb EMB120RT · Propeller Controlling System
  > AFTER TAKEOFF, NR 2 ENGINE NP VARIED FROM 98 TO 102.2 PERCENT. REPLACED PROPELLER CONTROL UNIT.
- [SDR COMA9810264](https://openairdocs.org/sdr/COMA9810264.md): Pcu · malfunction · Nov 13, 1998 · N246CA · Emb EMB120RT · Propeller Controlling System
  > RIGHT HAND NP VARIED BETWEEN 98 AND 102 PERCENT. REPLACED THE RIGHT HAND PROPELLER CONTROL UNIT.
- [SDR COMA9810215](https://openairdocs.org/sdr/COMA9810215.md): Bulb · failed · Sep 16, 1998 · N246CA · Emb EMB120RT · Emergency Lighting
  > 1ST OVERHEAD EMERGENCY LIGHT IS INOP. REPLACED BULB.
- [SDR COMA9810159](https://openairdocs.org/sdr/COMA9810159.md): Hose · loose · Jul 15, 1998 · N246CA · Emb EMB120RT · Cabin Cooling System
  > RIGHT HAND AIR CONDITIONING PACK FAILED AFTER TAKEOFF. TIGHTENED SEVERAL LOOSE HOSE CLAMPS AT RIGHT HAND AIRCRAFT PACK.
- [SDR COMA9710474](https://openairdocs.org/sdr/COMA9710474.md): Sensor · failed · Nov 10, 1997 · N246CA · Emb EMB120RT · Pneumatic Indicating System
  > LEFT HAND BLEED AIR DUCT LEAK WARNING ACTIVATED. REPLACED TWO DEFECTIVE LEAK WARNING SENSORS.
- [SDR COMA9710469](https://openairdocs.org/sdr/COMA9710469.md): Sig Cond Unit · malfunctioned · Nov 4, 1997 · N246CA · Emb EMB120RT · Propeller Controlling System
  > RIGHT HAND PROPELLER AUTOFEATHER SYSTEM IS INOP. REPLACED THE ENGINE SIGNAL CONDITIONER UNIT.
- [SDR COMA9710466](https://openairdocs.org/sdr/COMA9710466.md): Wire · shorted · Oct 26, 1997 · N246CA · Emb EMB120RT · Engine Indicating System Wiring
  > LEFT HAND TORQUE INDICATION IS ERRATIC. REPAIRED DAMAGED WIRE UNDER CABIN GALLEY FLOOR.
- [SDR COMA9710423](https://openairdocs.org/sdr/COMA9710423.md): Selector · malfunctioned · Oct 4, 1997 · N246CA · Emb EMB120RT · Landing Gear Selector
  > LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. ON THIRD ATTEMPT GEAR EXTENDED NORMAL. COULD NOT DUPLICATE DISCREPANCY. REPLACED LANDING GEAR SELECTER CONTROL BOX FOR TROUBLESHOOTING.
- [SDR COMA9710349](https://openairdocs.org/sdr/COMA9710349.md): Torque Sensor · inoperative · Aug 15, 1997 · N246CA · Emb EMB120RT · Engine BMEP/Torque Indicating
  > LEFT ENGINE TORQUE GAUGE READS ZERO. REMOVED AND REPLACED LEFT ENGINE TORQUE SENSOR WITH SERVICEABLE UNIT.
- [SDR COMA9710346](https://openairdocs.org/sdr/COMA9710346.md): Battery · discharged · Aug 9, 1997 · N246CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY EXIT LIGHTING INOP.
- [SDR COMA9710324](https://openairdocs.org/sdr/COMA9710324.md): Warning · malfunctioned · Jul 6, 1997 · N246CA · Emb EMB120RT · Door Warning System
  > CARGO DOOR WARNING AFTER TAKEOFF. NO DEFECT WITH DOOR. DOOR WARNING SYSTEM PLACED ON DEFERRED MAINTENANCE LIST.
- [SDR COMA9610226](https://openairdocs.org/sdr/COMA9610226.md): Reservoir · leaking · Jul 17, 1996 · N246CA · Emb EMB120RT · Hydraulic Reservoir, Main
  > LEFT HYDRAULIC RESERVOIR LOW PRESSURE WARNING ILLUMINATED DURING FLIGHT. REPLACED THE HYDRAULIC RESERVOIR ASSY.
- [SDR COMA9610193](https://openairdocs.org/sdr/COMA9610193.md): Valve · malfunction · Jun 24, 1996 · N246CA · Emb EMB120RT · Landing Gear Retraction/Extension System
  > WHEN LANDING GEAR SELECTED DOWN, BOTH LT A AND B SYSTEM INTRANSIT LIGHTS REMAINED ON. WHEN LANDING GEAR CYCLED, THE RT A AND B INTRANSIT LIGHTS REMAINED ON. REPLACED THE LANDING GEAR SOLENOID VALVE. PART TOTAL CYCLES, 7,283.
- [SDR COMA9610159](https://openairdocs.org/sdr/COMA9610159.md): Actuator · out of adjust · Jun 1, 1996 · N246CA · Emb EMB120RT · Landing Gear Actuator
  > WHEN LANDING GEAR SELECTED UP, THE LT MLG REMAINED DOWN FOR 5 MINUTES BEFORE RETRACTING. ADJUSTED RETRACT ACTUATOR TO M/M SPECIFICATIONS AND ACFT RETURNED TO SERVICE.
- [SDR COMA9610143](https://openairdocs.org/sdr/COMA9610143.md): Current Sensor · failed · May 11, 1996 · N246CA · Emb EMB120RT · Pitot/Static Anti-Ice System
  > NR 2 PITOT STATIC HEAT INOP WARNING ON. REPLACED THE NR 2 PITOT STATIC HEAT CURRENT SENSOR.
- [SDR COMA9610141](https://openairdocs.org/sdr/COMA9610141.md): Solenoid Valve · defective · May 5, 1996 · N246CA · Emb EMB120RT · Landing Gear Retraction/Extension System
  > WHEN LANDING GEAR SELECTED UP, THE LT MLG REMAINED DOWN. REPLACED THE LANDING GEAR SOLENOID VALVE.
- [SDR COMA9512044](https://openairdocs.org/sdr/COMA9512044.md): Tracks · dirty · Dec 27, 1995 · N246CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY, CLEANED FLAP TRACKS AND ACFT RETURNED TO SERVICE.
- [SDR COMA9512025](https://openairdocs.org/sdr/COMA9512025.md): Circuit Breaker · tripped · Dec 13, 1995 · N246CA · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice System
  > LEFT PROPELLER DE-ICE FAILED. RESET TRIPPED CIRCUIT BREAKER. SYSTEM CHECK NORMAL AND ACFT RETURNED TO SERVICE.
- [SDR COMA9512008](https://openairdocs.org/sdr/COMA9512008.md): Tiller · out of adjust · Nov 19, 1995 · N246CA · Emb EMB120RT · Landing Gear Steering System
  > NOSE WHEEL STEERING PULLS TO LEFT AND WILL NOT CENTER. PEDAL STEER INOP LIGHT IS ON. ADJUSTED THE STEERING TILLER LOAD POT. SYSTEM TEST SATISFACTORY.
- [SDR COM11922](https://openairdocs.org/sdr/COM11922.md): Select Lever · defective · Jun 23, 1995 · N246CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP CONTROL FAULT WARNING. REPLACED THE FLAP SELECTOR LEVER ASSY.
- [SDR COM11921](https://openairdocs.org/sdr/COM11921.md): Flap Handle · malfunctioned · Jun 15, 1995 · N246CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP WARNING SYSTEM INDICATED CONTROL FAULT MALFUNCTION THREE TIMES DURING DESCENT. REMOVED AND REPLACED FLAP CONTROL HANDLE WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.
- [SDR COM11906](https://openairdocs.org/sdr/COM11906.md): Annunciator · defective · May 30, 1995 · N246CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP CONTROL FAULT WARNING WHEN FLAPS SELECTED TO 25 DEGREES. REPLACED THE FLAP ANNUNCIATOR UNIT.
- [SDR COM11890](https://openairdocs.org/sdr/COM11890.md): Control Unit · defective · May 15, 1995 · N246CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP CONTROL FAULT WARNING WHEN FLAPS SELECTED TO 15 DEGREES. REPLACED THE FLAP CONTROL UNIT.
- [SDR COM11855](https://openairdocs.org/sdr/COM11855.md): Skin Supports · cracked · Apr 10, 1995 · N246CA · Emb EMB120RT · Wing, Plate/Skin
  > THE FOLLOWING PART NUMBER WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASKS 5720-551/651-01I AND 5720-552/652-01I. THE CRACKED WING SKIN SUPPORTS WERE REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NUMBER 1327-2. RIB SKIN SUPPORT PART NUMBERS 3 EA

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N246CA' AND deregistration_id = 'N246CA-2001-03-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N246CA-2001-03-30/reports

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